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DTIC AD0889049: Effects of Wing-Tip Fin and Nose Geometry on the Stability Characteristics of a Tow Target Configuration at Mach Numbers from 0.5 to 0.9

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DTIC AD0889049: Effects of Wing-Tip Fin and Nose Geometry on the Stability Characteristics of a Tow Target Configuration at Mach Numbers from 0.5 to 0.9

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Defense Technical Information Center

Publication date
Topics
DTIC Archive, Kaupp, H, ARO INC ARNOLD AFS TN, *AERIAL TARGETS, AERODYNAMIC CONTROL SURFACES, FINS, MODEL TESTS, PITCH(MOTION), STABILITY, SUBSONIC CHARACTERISTICS, TOWED BODIES, WIND TUNNEL MODELS, YAW,
Collection
dticarchive; additional_collections
Language
English
Aerodynamic stability and drag coefficients were obtained for five configurations of a 0.166-scale tow target at Mach numbers from 0.5 to 0.90. The primary configuration variables were tip fin size and fin cant angle. Effects of a blunted ogive nose as compared to an inlet shape nose were also investigated.
Addeddate
2019-12-07 07:33:05
Identifier
DTIC_AD0889049
Identifier-ark
ark:/13960/t4sj9m49j
Ocr
ABBYY FineReader 11.0 (Extended OCR)
Pages
40
Ppi
300
Year
1971

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